IT644011A - - Google Patents

Info

Publication number
IT644011A
IT644011A IT644011DA IT644011A IT 644011 A IT644011 A IT 644011A IT 644011D A IT644011D A IT 644011DA IT 644011 A IT644011 A IT 644011A
Authority
IT
Italy
Application number
Other languages
Italian (it)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Publication of IT644011A publication Critical patent/IT644011A/it

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT644011D 1960-02-01 IT644011A (US07235543-20070626-C00056.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US6001A US3061426A (en) 1960-02-01 1960-02-01 Creep resistant alloy

Publications (1)

Publication Number Publication Date
IT644011A true IT644011A (US07235543-20070626-C00056.png)

Family

ID=21718784

Family Applications (1)

Application Number Title Priority Date Filing Date
IT644011D IT644011A (US07235543-20070626-C00056.png) 1960-02-01

Country Status (10)

Country Link
US (1) US3061426A (US07235543-20070626-C00056.png)
BE (1) BE599751A (US07235543-20070626-C00056.png)
CH (1) CH403307A (US07235543-20070626-C00056.png)
DE (1) DE1238672B (US07235543-20070626-C00056.png)
FR (1) FR1280924A (US07235543-20070626-C00056.png)
GB (1) GB920551A (US07235543-20070626-C00056.png)
IT (1) IT644011A (US07235543-20070626-C00056.png)
NL (1) NL260545A (US07235543-20070626-C00056.png)
NO (1) NO102807L (US07235543-20070626-C00056.png)
SE (1) SE208441C1 (US07235543-20070626-C00056.png)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1053066A (US07235543-20070626-C00056.png) * 1963-07-19 1900-01-01
GB1075216A (en) * 1963-12-23 1967-07-12 Int Nickel Ltd Nickel-chromium alloys
US3411898A (en) * 1966-03-25 1968-11-19 Union Carbide Corp Nickel base alloy
US3642469A (en) * 1969-08-29 1972-02-15 Gen Electric High-stability nickel base alloy
GB1367661A (en) * 1971-04-07 1974-09-18 Int Nickel Ltd Nickel-chromium-cobalt alloys
USRE28681E (en) * 1973-04-02 1976-01-13 High temperature alloys
US3869284A (en) * 1973-04-02 1975-03-04 French Baldwin J High temperature alloys
US4053308A (en) * 1974-12-24 1977-10-11 Howmedica, Inc. Nonprecious alloy for fusion to porcelain
USRE29920E (en) * 1975-07-29 1979-02-27 High temperature alloys
DE3109293C2 (de) * 1980-03-13 1985-08-01 Rolls-Royce Ltd., London Verwendung einer Nickellegierung für einkristalline Gußstücke
US4624716A (en) * 1982-12-13 1986-11-25 Armco Inc. Method of treating a nickel base alloy
US4685977A (en) * 1984-12-03 1987-08-11 General Electric Company Fatigue-resistant nickel-base superalloys and method
US5130086A (en) * 1987-07-31 1992-07-14 General Electric Company Fatigue crack resistant nickel base superalloys
US5171380A (en) * 1987-07-31 1992-12-15 General Electric Company Method of forming fatigue crack resistant Rene' 95 type nickel base superalloys and product formed
US5130088A (en) * 1987-10-02 1992-07-14 General Electric Company Fatigue crack resistant nickel base superalloys
US5156808A (en) * 1988-09-26 1992-10-20 General Electric Company Fatigue crack-resistant nickel base superalloy composition
US5129970A (en) * 1988-09-26 1992-07-14 General Electric Company Method of forming fatigue crack resistant nickel base superalloys and product formed
US5129971A (en) * 1988-09-26 1992-07-14 General Electric Company Fatigue crack resistant waspoloy nickel base superalloys and product formed
US5129968A (en) * 1988-09-28 1992-07-14 General Electric Company Fatigue crack resistant nickel base superalloys and product formed
US5129969A (en) * 1988-09-28 1992-07-14 General Electric Company Method of forming in100 fatigue crack resistant nickel base superalloys and product formed
US5055147A (en) * 1988-12-29 1991-10-08 General Electric Company Fatigue crack resistant rene' 95 type superalloy
US5130089A (en) * 1988-12-29 1992-07-14 General Electric Company Fatigue crack resistant nickel base superalloy
US4983233A (en) * 1989-01-03 1991-01-08 General Electric Company Fatigue crack resistant nickel base superalloys and product formed
US5143563A (en) * 1989-10-04 1992-09-01 General Electric Company Creep, stress rupture and hold-time fatigue crack resistant alloys
US5360496A (en) * 1991-08-26 1994-11-01 Aluminum Company Of America Nickel base alloy forged parts
US5374323A (en) * 1991-08-26 1994-12-20 Aluminum Company Of America Nickel base alloy forged parts
US5476555A (en) * 1992-08-31 1995-12-19 Sps Technologies, Inc. Nickel-cobalt based alloys
US6521175B1 (en) 1998-02-09 2003-02-18 General Electric Co. Superalloy optimized for high-temperature performance in high-pressure turbine disks
US6974508B1 (en) 2002-10-29 2005-12-13 The United States Of America As Represented By The United States National Aeronautics And Space Administration Nickel base superalloy turbine disk
US20100008790A1 (en) * 2005-03-30 2010-01-14 United Technologies Corporation Superalloy compositions, articles, and methods of manufacture
ES2269013B2 (es) 2006-12-01 2007-11-01 Industria De Turbo Propulsores, S.A. Superaleaciones monocristalinas y solidificadas direccionalmente de baja densidad.
US9752215B2 (en) 2012-02-14 2017-09-05 United Technologies Corporation Superalloy compositions, articles, and methods of manufacture
US9783873B2 (en) 2012-02-14 2017-10-10 United Technologies Corporation Superalloy compositions, articles, and methods of manufacture
JP6213185B2 (ja) * 2013-11-25 2017-10-18 株式会社Ihi ニッケル基合金
WO2017189208A1 (en) 2016-04-27 2017-11-02 Siemens Energy, Inc. Gas turbine blade with corrugated tip wall
US10793934B2 (en) 2017-05-02 2020-10-06 United Technologies Corporation Composition and method for enhanced precipitation hardened superalloys

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB583807A (en) * 1943-06-30 1946-12-31 Harold Ernest Gresham Nickel base alloy
FR1071278A (fr) * 1951-12-05 1954-08-30 Mond Nickel Co Ltd Perfectionnements aux alliages résistant à la chaleur et objets et pièces fabriqués à partir desdits alliages
US2920956A (en) * 1956-10-08 1960-01-12 Universal Cyclops Steel Corp Method of preparing high temperature alloys
US2912323A (en) * 1957-09-16 1959-11-10 Int Nickel Co Cast nickel base alloy for high temperature service

Also Published As

Publication number Publication date
NO102807L (US07235543-20070626-C00056.png)
US3061426A (en) 1962-10-30
FR1280924A (fr) 1962-01-08
NL260545A (US07235543-20070626-C00056.png)
GB920551A (en) 1963-03-06
BE599751A (US07235543-20070626-C00056.png)
CH403307A (fr) 1965-11-30
SE208441C1 (US07235543-20070626-C00056.png) 1966-10-25
DE1238672B (de) 1967-04-13

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